[Reports] / Amer.inst.of aeronautics and astronautics. N 89-2805 : Numerical analysis of supersonic flow through oscillating cascade sections by using a deforming grid : Rev.presented at the AIAA/ASME/SAE/ASEE 25th joint propulsion conf., Jul.10-12, 1989, Monterey(Ca) / D.L.Huff,T.S.R.Reddy, 1988. - 15 p. - Текст : непосредственный.
Application of an efficient hybrid scheme for aeroelastic analysis of advanced propellers : Rev.presented at the 28th aerospace sciemces meet, Jan.8-11, 1990, Reno(Nv) / R.Srivastava,N.L.Sankar,T.S.R.Reddy,D.L.Huff, 1990. - 28 p. - Текст : непосредственный.